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Aircraft record

N405AE2000 Eurocopter AS 350 B3

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:1 NTSB accident (substantial damage, Sep 2000)5 ADs may apply8 service difficulty reports

Registration
Valid
expires Apr 30, 2028
Based in
Ketchikan, AK
owner city / state
Engine
ARRIEL 1SER · 681 hp
Turbomeca
Owners
1
since 2000
NTSB events
1
substantial, 2000
ADs may apply
5
confirm with A&P
Service reports
8
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
Temsco Helicopters INC
Owner type
Corporation
City, state
Ketchikan, AK
Certificate issued
Sep 22, 2000
Expires
Apr 30, 2028
Airworthiness
Standard · Normal
Airworthiness date
Aug 15, 2000

We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.

Airframe & engine

FAA Registry + type data

Airframe

Manufacturer
Eurocopter
Model
AS 350 B3
Year
2000
Serial number
3286
Aircraft type
Rotorcraft
Category
Land
Certification
Type Certificated
Seats
6
Engines
1
Max takeoff weight
Up to 12,499 lb
Type certificate data sheet
H9EU
Mode S code
A4BF39

Engine

Make and model
Turbomeca Arriel 1ser
Type
Turbo-shaft
Power
681 hp

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 2000 – nowTemsco Helicopters INCKetchikan, AK · current

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026

NTSB events (1)

Accident · substantial damage

Sep 23, 2000 · Ketchikan, AK

The pilot's inadvertent activation of the collective flight stop/emergency fuel augmentation switch, which resulted in engine and main rotor overspeeds, thereby precipitating failures of the tail rotor drive shaft coupling and power turbine blades. A factor associated with the accident was the manufacturer's inadequate design of the flight stop switch, which has insufficient safeguards to…

Damage
Substantial
Injuries
None
Report
ANC00LA132

From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC00LA132)

Accident history for this model

ADs published since 1998 that may apply (5)

These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.

ADSubjectEffectiveApplies to
2021-04-15Vertical Stabilizer, Spar/RibMar 23, 2021Airframe (AS 350 B3)Only with: AS350B3 helicopters excluded if Modification 07.3148 embodied in production or Eurocopter AS350 Service Bulletin 55.00.14 (any revision) embodied in service; AS355 models all serial numbers.
2013-23-09Eurocopter France HelicoptersDec 27, 2013Airframe (AS 350 B3)Only with: Helicopters with sliding doors installed, except those with modification AL.4262.
2013-21-01Eurocopter France (Eurocopter) HelicoptersOct 25, 2013Airframe (AS 350 B3)Only with: Tail rotor hub pitch horn assembly P/N 350A121368.01, .02, .03, or .04, with pitch horn P/N 350A121368.XX, installed.
2013-08-19Eurocopter France HelicoptersJun 5, 2013Airframe (AS 350 B3)Only with: Sliding door pre-modification (MOD) 073298 or pre-MOD 073308 installed.
2012-25-04Eurocopter France HelicoptersMay 9, 2013Airframe (AS 350 B3)Only with: Modification (MOD) 07 5601 installed (AS350B3e configuration).

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (8)

Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.

  • Engine · ring · crackedMar 2, 2006

    IN COMPLIANCE WITH AD AND SB, OUR MECHANIC WAS INSPECTING THE ABOVE DESCRIBED ENGINE AND FOUND THE COMPONENT LISTED BELOW TO BE OUT OF SERVICEABLE LIMITS AS INDICATED IN THE 2 DOCUMENTS. REMOVED THE CONTAINMENT RING FROM SERVICE AND INSTALLED A NEW POST MOD TU-22 RING AS ADVISED. (K)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Tail rotor · blade · crackedMay 7, 2004

    INSPECTOR FOUND CRACK IN TAIL ROTOR PROTRUDING OUT OF RIVET LOCATION ON TRIM TAB. CRACK WAS FOUND DURING INSPECTION IAW AD 2001-26-55. (AL05200402466)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine controls · roll pin · failedJul 18, 2003

    AIRCRAFT FAILED POWER CHECKS DUE TO TORQUE FAILURE. INVESTIGATED SITUATION AND DETERMINED THAT A ROLL PIN FAILURE HAD OCCURED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 8 reports
  • Fuselage · structure · buckledOct 14, 2002

    FUSELAGE BOX STRUCTURE CROSS BRACES BUCKLED. SENT FOR JIG SET AND REPAIR.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine indicating · module · failedSep 18, 2002

    TORQUE INDICATION STARTED TO FLUCTUATE, AIRCRAFT GROUNDED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine indicating · module · failedJul 10, 2002

    TORQUE INDICATION STARTED TO FLUCTUATE. REMOVED MO1 MODULE WHICH HOURS THE TORQUE TUBE AND INSTALLED RENTAL MODUAL, SENT MO1 TO MFG. THIS WAS THEIR RENTAL. THEY DID NOTIFICATION THAT THIS WAS THE SAME TYPE OF FAILURE BEFORE IN THE FACT THAT THE ROLL PINS ON THE TORQUE TUBE HAD SHEARED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine indicating · module · failedJun 18, 2002

    REMOVED ENGINE MODULE 1 DUE TO TORQUE SYSTEM REFERENCE SHAFT PHONIC WHEEL ROLL PINS SHEARING CAUSING LOSS OF TORQUE INDICATION VEMD. REMOVED LOANER MODULE 1 FOR REPAIR. INSTALLED LOANER MODULE. SENDING UNIT TO MFG FOR REPAIR.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine indicating · module · failedJun 5, 2002

    TORQUE INDICATION STARTED TO FLUCTUATE. REMOVED NR 1 MODULE WHICH HOUSES THE TORQUE TUBE AND INSTALLED A RENTAL. SENT NR 1 OUT FOR REPAIR. IT WAS DETERMINED THAT THE ROLL PINS IN TORQUE TUBE HAD SHEARED OFF.

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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